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Climb Performance of a Piston-Propeller Airplane with Cambered Wing and Variable Propeller Efficiency

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dc.contributor.authorCavcar, Aydan
dc.date.accessioned2025-11-13T12:16:56Z
dc.date.issued2011-09-01
dc.identifier.doihttps://doi.org/10.2514/1.c031351
dc.identifier.endpage1707
dc.identifier.issn0021-8669
dc.identifier.issue5
dc.identifier.openalexW2157521391
dc.identifier.startpage1701
dc.identifier.urihttps://hdl.handle.net/11421/9539
dc.identifier.urihttps://doi.org/10.2514/1.c031351
dc.identifier.volume48
dc.language.isoen
dc.relation.ispartofJournal of Aircraft
dc.rightsrestrictedAccess
dc.subjectAirplane
dc.subjectClimb
dc.subjectPropeller
dc.subjectWing
dc.subjectMarine engineering
dc.subjectPiston (optics)
dc.subjectAerospace engineering
dc.subjectAeronautics
dc.subjectEngineering
dc.subjectWing loading
dc.subjectWing configuration
dc.subjectAdvance ratio
dc.subjectAngle of attack
dc.subjectPhysics
dc.subjectBlade pitch
dc.subjectAerodynamics
dc.subjectTurbine
dc.subject.sdg7
dc.titleClimb Performance of a Piston-Propeller Airplane with Cambered Wing and Variable Propeller Efficiency
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5023712238

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